Crashworthiness optimization of corrugated sandwich panels

被引:121
作者
Hou, Shujuan [1 ,2 ]
Zhao, Shuyun [1 ,2 ]
Ren, Lili [1 ,2 ]
Han, Xu [1 ,2 ]
Li, Qing [3 ]
机构
[1] Hunan Univ, State Key Lab Adv Design & Mfg Vehicle Body, Changsha 410082, Hunan, Peoples R China
[2] Hunan Univ, Coll Mech & Vehicle Engn, Changsha 410082, Hunan, Peoples R China
[3] Univ Sydney, Sch Aerosp Mech & Mechatron Engn, Sydney, NSW 2006, Australia
基金
中国国家自然科学基金;
关键词
Crashworthiness; Optimization; Sandwich panel; Corrugated core; Energy absorption; MULTIOBJECTIVE OPTIMIZATION; IMPACT DAMAGE; DESIGN; FAILURE; SHEET;
D O I
10.1016/j.matdes.2013.04.086
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
As a class of important lightweight structural components, sandwich panels have gained considerable popularity in a range of engineering applications. The crashworthiness of sandwich structures, which signifies a key mechanical property under impact loading, is found largely related to shape and dimensional parameters, such as cell width, wall thickness, structural angle and core height. This study exemplifies corrugated sandwich panels with trapezoidal and triangular cores to determine the relationship between the structural parameters and the crashworthiness under low-velocity local impact and planar impact, further optimizing these structural parameters with the crashworthiness criteria by using multiobjective optimization techniques. The configurations of trapezoidal and triangular core cells are firstly optimized for maximizing energy absorption. The wall thickness of sandwich panels with optimal trapezoidal core shape is then optimized for crashworthiness. Finally, the crashworthiness of these two types of corrugated sandwich panels is compared with each other under the identical face sheet thickness and core density and it is found that the triangular configuration has better performance. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1071 / 1084
页数:14
相关论文
共 32 条
[1]   Prediction of impact damage on sandwich composite panels [J].
Aktay, L ;
Johnson, AF ;
Holzapfel, M .
COMPUTATIONAL MATERIALS SCIENCE, 2005, 32 (3-4) :252-260
[2]  
Atli-Veltin B, 2010, P 66 AM HEL SOC ANN, P206
[3]   Impact damage processes in composite sheet and sandwich honeycomb materials [J].
Dear, JP ;
Lee, H ;
Brown, SA .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2005, 32 (1-4) :130-154
[4]   Dynamic response of a multilayer prismatic structure to impulsive loads incident from water [J].
Dharmasena, Kumar ;
Queheillalt, Doug ;
Wadley, Haydn ;
Chen, Yungchia ;
Dudt, Philip ;
Knight, David ;
Wei, Zhensong ;
Evans, Anthony .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2009, 36 (04) :632-643
[5]   A comparative study of metamodeling methods for multiobjective crashworthiness optimization [J].
Fang, H ;
Rais-Rohani, M ;
Liu, Z ;
Horstemeyer, MF .
COMPUTERS & STRUCTURES, 2005, 83 (25-26) :2121-2136
[6]   Evaluation of response surface methodologies used in crashworthiness optimization [J].
Forsberg, J ;
Nilsson, L .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2006, 32 (05) :759-777
[7]   Topological optimization of rotorcraft subfloor structures for crashworthiness considerations [J].
Hajela, P ;
Lee, E .
COMPUTERS & STRUCTURES, 1997, 64 (1-4) :65-76
[8]  
Hallquist J., 2014, LS-DYNA keyword user's manual, Version 971
[9]  
Hallquist JO., 2006, LS DYNA THEORETICAL
[10]   Computational methods for bird strike simulations: A review [J].
Heimbs, Sebastian .
COMPUTERS & STRUCTURES, 2011, 89 (23-24) :2093-2112